CN201350345Y - Main shaft supporting structure of model helicopter - Google Patents
Main shaft supporting structure of model helicopter Download PDFInfo
- Publication number
- CN201350345Y CN201350345Y CNU2008202065443U CN200820206544U CN201350345Y CN 201350345 Y CN201350345 Y CN 201350345Y CN U2008202065443 U CNU2008202065443 U CN U2008202065443U CN 200820206544 U CN200820206544 U CN 200820206544U CN 201350345 Y CN201350345 Y CN 201350345Y
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- CN
- China
- Prior art keywords
- main shaft
- bearing
- model
- supporting structure
- shaft supporting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses a main shaft supporting structure of a model helicopter, comprising a main shaft. The upper end and the lower end of the main shaft are symmetrically provided with an upper bearing seat and a lower bearing set. A ball bearing which can bear the radial loading and a thrust bearing which can bear the axial loading are arranged in the bearing seat. The thrust bearing is arranged under the bearing of the original main shaft, and the trust bearing bears the axial loading produced by the ascending and the descending of the model helicopter, thereby, the service life of the main shaft bearing of the model helicopter is ensured, the movement of the main shaft is smoother and more flexible and the efficiency is improved.
Description
Technical field
The utility model relates to the main shaft supporting structure of a kind of model copter, particularly a kind of model copter.
Background technology
Along with the quickening of urban development, like thereby make remote control model helicopter more and more be subjected to the model fan.The mast of traditional model copter is usually by two plain ball bearings supports up and down, but because model copter need rise and decline even inverted flight, continuous change direction of axial load and dynamics, thereby cause main shaft bearing not only to be subjected to main oar action of centrifugal force, also be subjected to the axial force of bringing of the lift of main oar generation, plain bearing can bear certain axial force, but varying loading can make the main shaft bearing duty worsen and too fast damage for a long time, so develop the research schedule that a kind of main shaft supporting structure that can effectively bear axial load has been put on people.
Summary of the invention
In order to overcome the deficiencies in the prior art, the utility model provides a kind of model copter main shaft supporting structure that effectively bears the main shaft axial force.
The technical scheme that its technical problem that solves the utility model adopts is:
A kind of main shaft supporting structure of model copter comprises main shaft, and the upper and lower end of described main shaft is symmetrically arranged with upper and lower bearing block, is provided with ball bearing that can bear radial load and the thrust bearing that can bear axial load in the described bearing block;
As further improvement in the technical proposal, the inner ring and the thrust bearing of described ball bearing are in contact with one another.
The beneficial effects of the utility model are: this product mainly is to be provided with thrust bearing under the bearing of former main shaft, bear the axial load that model copter rises and descends and produce by thrust bearing, thereby guarantee the service life of the bearing of model copter main shaft, and make motion of main shaft more smooth and easy flexibly, improved efficiency.
Description of drawings
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is a structural representation of the present utility model.
The specific embodiment
With reference to Fig. 1, a kind of main shaft supporting structure of model copter, comprise main shaft 1, the upper and lower end of described main shaft 1 is symmetrically arranged with upper and lower bearing block 2, be provided with plain ball bearing 3 that bears radial load and the thrust bearing 4 that bears axial load in the described bearing block 2, in order to reach result of use, the tight ring end face of the inner ring of described ball bearing 3 and thrust bearing 4 is in contact with one another.
This product mainly is to have increased thrust bearing 4 on former main shaft, removes to bear the axial load that model copter rises and descends and produce by thrust bearing, guarantees the service life of model copter main shaft bearing, makes motion of main shaft more flexible.
Claims (2)
1. the main shaft supporting structure of a model copter, comprise main shaft (1), it is characterized in that: the upper and lower end of described main shaft (1) is symmetrically arranged with upper and lower bearing block (2), be provided with in the described bearing block (2) ball bearing (3) that can bear radial load and only with bear axial load thrust bearing (4).
2. the main shaft supporting structure of a kind of model copter according to claim 1, it is characterized in that: the inner ring of described ball bearing (3) and thrust bearing (4) are in contact with one another.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008202065443U CN201350345Y (en) | 2008-12-31 | 2008-12-31 | Main shaft supporting structure of model helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008202065443U CN201350345Y (en) | 2008-12-31 | 2008-12-31 | Main shaft supporting structure of model helicopter |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201350345Y true CN201350345Y (en) | 2009-11-25 |
Family
ID=41373733
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNU2008202065443U Expired - Fee Related CN201350345Y (en) | 2008-12-31 | 2008-12-31 | Main shaft supporting structure of model helicopter |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN201350345Y (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102500271A (en) * | 2011-10-12 | 2012-06-20 | 河南科技大学 | Load-bearing bearing for slurry mixing equipment |
CN108973664A (en) * | 2018-06-13 | 2018-12-11 | 泰安九洲金城机械有限公司 | A kind of transmission shaft support device, transmission system and vehicle |
-
2008
- 2008-12-31 CN CNU2008202065443U patent/CN201350345Y/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102500271A (en) * | 2011-10-12 | 2012-06-20 | 河南科技大学 | Load-bearing bearing for slurry mixing equipment |
CN102500271B (en) * | 2011-10-12 | 2014-02-26 | 河南科技大学 | Load-bearing bearing for slurry mixing equipment |
CN108973664A (en) * | 2018-06-13 | 2018-12-11 | 泰安九洲金城机械有限公司 | A kind of transmission shaft support device, transmission system and vehicle |
CN108973664B (en) * | 2018-06-13 | 2019-05-03 | 泰安九洲金城机械有限公司 | A kind of transmission shaft support device, transmission system and vehicle |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091125 Termination date: 20131231 |